Title:
GUIDED MISSILE
Document Type and Number:
Japanese Patent JPS53131700
Kind Code:
A
Abstract:
PURPOSE: To provide guided missile which has variable aileron forwards from center of gravity, the aileron is extended to change lift coefficient corresponding to change of center of gravity, to compensate guide control characteristics change by gravity center change of missile.
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Inventors:
NAGAI RIYUUICHI
MARUYAMA KATSUYOSHI
IGA HISASHI
MARUYAMA KATSUYOSHI
IGA HISASHI
Application Number:
JP4499077A
Publication Date:
November 16, 1978
Filing Date:
April 19, 1977
Export Citation:
Assignee:
MITSUBISHI ELECTRIC CORP
International Classes:
B64C5/18; B64C13/16; F42B15/00; (IPC1-7): B64C13/16